It can be calculated only if you got serious/manufacturer data inputs…
Graph, Horde attached is interesting but one expects more from Lockheed…all cited a/c has about the same curve slope vs Mach number ??
Like all has the same drag and thrust peaks…in reality some are better subsonic, other trans-sonic, supersonic…here MiG-29 has, it seems, fixed geometry inlets, max speed ~ Mach 2, sonic acc worse than F-16, fine propaganda move and effective.

I find MiG-21/F-4 Phantom supersonic instantaneous/sustained g/acceleration in one book at Amazon about their performance.
I reckon, besides confidentiality, manufacturers hide data if shamed of